Aquila AT01, Maintenance Manual

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MAINTENANCE MANUAL
AQUILA AT01
A
Page 23
05-20-00
16.09.19
Maintenance Checks
No. Inspection Items Inspection Finding / Initials
Control Surfaces Method Condition (Cont.)
40. Condition of hinges (bushings), corrosion, play. V
41. Inspect for previously performed repairs and repaintings. V
If so, check elevator mass and static moment to be within
specified limits (refer to 55-20-00).
42. Bolts at inner hinge - Check for condition, cracks, corrosion, V
thread.
No. Inspection Items Inspection Finding / Initials
Horizontal Stabilizer Method Condition
1. Stabilizer surfaces - Check for delamination of shells, scratches. V, T
2. Paint surfaces - Check for condition, scratches, UV damage, V
chipping of paint.
3. Damage of core, dents in core, disbond between core and skin. V, T
4. Stabilizer leading edges - Check for bonding delamination. V, T
5. Trailing edge spar - Check for cracks and bonding V, T
delamination with skin.
6. Areas around hinge supports in trailing edge spar - Check V
for cracks and delamination.
7. Condition of hinges (bushings), corrosion, play. V
No. Inspection Items Inspection Finding / Initials
Fuselage Method Condition
Fuselage Skin Structure and Vertical Stabilizer Skin
1. Skin surfaces - Check for delamination of shells, scratches. V, T
2. Paint surfaces - Check for condition, scratches, UV damage, V
chipping of paint.
3. Damage of core, dents in core, disbond between core and skin. V, T
4. Areas near bonding seam at centerline on upper and lower V, T
fuselage surfaces - Inspect for cracks in paint.
5. Check condition of drain holes in lower fuselage. V
6. Inspect for previously performed repairs and repaintings. V
7. Areas near bonding seam at connection between horizontal V
and vertical stabilizer on upper and lower horizontal surfaces -
Inspect for cracks in paint.